[Isocops] IBEX Orbit# 228 SSR_Dump/Tracking Contact 8 Dec 13

[Ibex Mission Operations]

The SSR_Dump/Tracking Contact for Orbit# 228 was nominal for
command/telemetry and the inertial maneuver successful.
The following objectives are accomplished

1. reset_master_timer.scr
2.SSR_Dump.sce (new)
3.CAR# 658 Upload Orbit# 229 IBEX_Hi Gain Test
IBEX_2013_342_o0229a_hgc_v001.scr (301-363)
4.ops_set_sc_time.scr



IBEX Orbit# 288 PERIGEE Target Vectors 8 Dec 13

  J2000  Spin Axis

  ECI X    -0.278343

  ECI Y    -0.881899

  ECI Z    -0.380498



  Precession Maneuver

  MPS Diff             0.735      deg

   * MPS Diff should be < 1.5 *



  0.51742600         ActNor.EstInrToBdy[0]

  0.65001500         ActNor.EstInrToBdy[1]

  -0.51957300       ActNor.EstInrToBdy[2]

  0.19948600         ActNor.EstInrToBdy[3]

   1070550000.000               ActNor.EstTime



  Right Ascension - RA          252.483 deg

  Declination - DEC                -22.365  deg



  IBEX Spin Axis vs. Sun Vector

  IBEX Sun Angle  -2.863    deg



  Orbit# 228 MPS Generated PERIGEE Target Vectors

  MPS Cmd Vector X             -0.273158000

  MPS Cmd Vector Y             -0.878577000

  MPS Cmd Vector Z             -0.391775000


    CSS Angle TLM 2.33003  CSS Sun-Pointing Angle 4.66006  05 Dec 13 @2329 CSS
Angle TLM 1.08137  CSS Sun-Pointing Angle 2.16274  08 Dec 13 @1500
*Pre-Burn*     Thruster 1 9360 05 Dec 13 @2329 Thruster 2 9136  Thruster 3
9856  Thruster 4 10080  *Post-Burn*   Thruster 1 9648 08 Dec 13 @1500 Thruster
2 9424  Thruster 3 10160  Thruster 4 10384  *Number of Pulses*    Thruster 1
288  Thruster 2 288  Thruster 3 304  Thruster 4 304  *Thruster Pairs*
 Thruster
1 & 2 576  Thruster 3 & 4 608


-- 
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
CYGNUS Mission Planning
(304) 279-6678
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